Experimental investigation of rolling moment for a body-wing-tail missile configuration with wrap around wings and straight tails at supersonic speeds
10th Atmospheric Flight Mechanics Conference ; 1983 ; Gatlinburg , TN , U.S.A.
01.01.1983
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Wing-body interference at supersonic speeds with application to combinations with rectangular wings
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